Whether you are in need of military aviation parts, NSN components, or various forms of aerospace and defense parts, Aerospace Store is a single-sourcing solution with over 2 billion product listings readily available for purchase at any time with competitive pricing. You have reached the Request for Quote (RFQ) page for part number 4083210, a Samsung Techwin Co Ltd component we feature that is listed with the NSN 2840014487540 and item name “Case Turbine Aircraft Gas Turbin.” For further identification, part number 4083210 was also specifically produced under CAGE Code 1645F and belongs to Federal Supply Class (FSC) 2840 Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components. If you would like to receive specific options for procurement that have been tailored to your unique needs and restrictions alike, we ask that you please fill out and submit the form provided on this page with as much information as you can. Once our team has a chance to receive and review your offered details, a dedicated account manager will be in touch shortly after.
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| NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
|---|---|---|---|---|---|---|
| 2840-01-448-7540 Item Description: Case Turbine Aircraft Gas Turbin | 2840 | 014487540 | 0 | N | ||
| CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
| I | A | 0 | ||||
| Part Number | isc | rnvc | rncc | HCC | MSDS | SADC |
| 4083210 | 5 | 2 | 3 |
| MRC | Criteria | Characteristic |
|---|---|---|
| ABHP | OVERALL LENGTH | 5.809 INCHES MINIMUM AND 5.813 INCHES MAXIMUM |
| ABMZ | DIAMETER | 28.330 INCHES MINIMUM AND 28.350 INCHES MAXIMUM |
| AGAV | END ITEM IDENTIFICATION | F100-PW-229 AIRCRAFT GAS TURBINE ENGINE |
| APGF | DESIGN TYPE | AXIAL COMPRESSOR |
| CRTL | CRITICALITY CODE JUSTIFICATION | CZBJ AND ABMZ AND ABHP AND FEAT |
| CZBJ | ENGINE SECTION LOCATION | TURBINE |
| FEAT | SPECIAL FEATURES | NT.O. 2J-F100-54, FIG 89, IND 71; USE ONLY ON P/N 4084522-800, -801, -802, 4082654-803, AND 4082657-808; LOCATION NEAR NO. 4 BEARING FRONT AIR SEALING RING, FRONT SEAL ASSY, COMPRESSOR EXIT STATOR AND DIFFUSER CASE |
| MATT | III MATERIAL | NICKEL ALLOY OVERALL |
| MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | PWA1010 MFR REF SINGLE MATERIAL RESPONSE OVERALL |
| ABHP | OVERALL LENGTH | 5.809 INCHES MINIMUM AND 5.813 INCHES MAXIMUM |
| ABMZ | DIAMETER | 28.330 INCHES MINIMUM AND 28.350 INCHES MAXIMUM |
| AGAV | END ITEM IDENTIFICATION | F100-PW-229 AIRCRAFT GAS TURBINE ENGINE |
| APGF | DESIGN TYPE | AXIAL COMPRESSOR |
| CRTL | CRITICALITY CODE JUSTIFICATION | CZBJ AND ABMZ AND ABHP AND FEAT |
| CZBJ | ENGINE SECTION LOCATION | TURBINE |
| FEAT | SPECIAL FEATURES | NT.O. 2J-F100-54, FIG 89, IND 71; USE ONLY ON P/N 4084522-800, -801, -802, 4082654-803, AND 4082657-808; LOCATION NEAR NO. 4 BEARING FRONT AIR SEALING RING, FRONT SEAL ASSY, COMPRESSOR EXIT STATOR AND DIFFUSER CASE |
| MATT | III MATERIAL | NICKEL ALLOY OVERALL |
| MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | PWA1010 MFR REF SINGLE MATERIAL RESPONSE OVERALL |
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